Indigo Questions

(1)

First few questions were of Air Regulation:

. Height and radius of VFR in congested Areas

. Fl to be

. Fl to be flown in case of unlawful interferenceflown in case of unlawful interference

. Fl to be

. Fl to be flown, True Heading was given along withflown, True Heading was given along with

variation and deviation, but what flight, VFR or IFR

wasn't given.

. Steady green light when a/c is on ground

. Series of red lights whn a/c is in flight

. Two questions were there on the radio failure in

. Two questions were there on the radio failure in IFR.IFR.

Meteorology

. Conditions in front of

. Conditions in front of Stationary FrontStationary Front

. Chart was given with Isobars and fronts along with TAF

clearly showing features of cold front, had identify the

station

Human Performance

. Two questions on stress a

. What behavior is not good in team work

. Alcohol is fi

. Alcohol is filtered by which organltered by which organ

Navigation

. What is the Chart length between 180E and 180W on

same lat .

. Chart length was given on 59 lat, w

. Chart length was given on 59 lat, what is the charthat is the chart

length on some other lat

. Three Alternates were given with the course and the

wind component, which alternate is close in terms of

time

. A to B

. A to B distance was given and wind component, whatdistance was given and wind component, what

is the total ti

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. What is the GS and Heading, Course and Wind

component were given

. QNH of ground is 1023 and elevation is 1500, how

much you have to climb for FL 750

. In Mercator chart RL is

. In Mercator chart RL is a straight or curved line ?a straight or curved line ?

. What is the Drift on **lat?

. What is the dis

. What is the distance when an A/C descends 15000ft attance when an A/C descends 15000ft at

the rate of 1500ft/min

. Radio Altimeter turns Analog to Circular at - a.

. Radio Altimeter turns Analog to Circular at - a. belowbelow

1000ft, b. at or below 1000ft, c. at

1000ft, b. at or below 1000ft, c. at DH.DH.

. One Altimeter is cal

. One Altimeter is calibrated for Inst./Pos. error andibrated for Inst./Pos. error and

other 1 is not, what happens is IAS changes

. Power of NDB is 100KW what is the range?

Technical

. Increase in al

. Increase in altitude but Angle of Attack, mass and IAStitude but Angle of Attack, mass and IAS

remains same, what happens to the Angle of Climb

. With Increase in al

. With Increase in altitude what happens to the TAS andtitude what happens to the TAS and

Drag

Hey can u please explain me the

solution for this question..

You are flying at FL 160. Outside air

temperature is -27° C, and the

pressure at sea level is 1003 hPa.

What is the true altitude?

A) 15090 feet. A) 15090 feet. B) 16910 feet. B) 16910 feet. C) 15630 feet. C) 15630 feet. D) 16370 feet. D) 16370 feet. Ans is (A) 15090 Ans is (A) 15090

(3)

. What is the GS and Heading, Course and Wind

component were given

. QNH of ground is 1023 and elevation is 1500, how

much you have to climb for FL 750

. In Mercator chart RL is

. In Mercator chart RL is a straight or curved line ?a straight or curved line ?

. What is the Drift on **lat?

. What is the dis

. What is the distance when an A/C descends 15000ft attance when an A/C descends 15000ft at

the rate of 1500ft/min

. Radio Altimeter turns Analog to Circular at - a.

. Radio Altimeter turns Analog to Circular at - a. belowbelow

1000ft, b. at or below 1000ft, c. at

1000ft, b. at or below 1000ft, c. at DH.DH.

. One Altimeter is cal

. One Altimeter is calibrated for Inst./Pos. error andibrated for Inst./Pos. error and

other 1 is not, what happens is IAS changes

. Power of NDB is 100KW what is the range?

Technical

. Increase in al

. Increase in altitude but Angle of Attack, mass and IAStitude but Angle of Attack, mass and IAS

remains same, what happens to the Angle of Climb

. With Increase in al

. With Increase in altitude what happens to the TAS andtitude what happens to the TAS and

Drag

Hey can u please explain me the

solution for this question..

You are flying at FL 160. Outside air

temperature is -27° C, and the

pressure at sea level is 1003 hPa.

What is the true altitude?

A) 15090 feet. A) 15090 feet. B) 16910 feet. B) 16910 feet. C) 15630 feet. C) 15630 feet. D) 16370 feet. D) 16370 feet. Ans is (A) 15090 Ans is (A) 15090

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How are we getting 15090??

18th May 2011, 18:06 18th May 2011, 18:06 # # (( ))

planeboy_777

Join Date: Aug 2010 Join Date: Aug 2010 Location: mumbai Location: mumbai Age: 21 Age: 21 Posts: 84 Posts: 84 True altitude = True altitude = Indicated altitude Indicated altitude + (ISA dev x 4 x + (ISA dev x 4 x Thousands of feet) Thousands of feet) = 16000 + (-10 x = 16000 + (-10 x 4 x 16) 4 x 16) = 16000+(-640) = 16000+(-640) = 16000-640 = 16000-640 = 15360ft (on = 15360ft (on 1013.25) 1013.25) Height difference is Height difference is 1013-1003=10Hpa 1013-1003=10Hpa therefore 10Hpa x therefore 10Hpa x 30= 300ft of height 30= 300ft of height difference between difference between 1013 and 1003 1013 and 1003 so 15360ft-300ft= so 15360ft-300ft= 15060FT(1003hpa) 15060FT(1003hpa) silly numerical silly numerical man!!! man!!! you made me you made me remember my remember my primar primar

(5)

Regs:

DGCA stuff, squawk code, type of transponder, class 'B'

VFR above 10,000MSL etc.

Met

Find height of tropopause from charts

Lapse rate questions

A/C flying south in southern hemi with stbd drift, which

pressure is it flying into?

What is pressure alt?

when are pressure alt n density alt same?

Human Performance

Stress

Rate of alcohol consumption in body

Middle and inner ear related questions

Eye questions including fovea and rods

Nav

Diagrams of AH and you have to identify the one with

the given condition

Altimeter numerical

flying from A to B, speed 0.84M. Distance 300nm, you

have to increase your ETA by 2min, when will you

decrease your speed? Previous ETA was given

Speed/Time problems

Gyro

Local time numerical

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Tech

AOA questions

time &rel velocities

hysterisis error

combination of what all site errors adf has

topple of DGI at pole

topple/wander of DGI at somewhere else on earth

where does the wing mounted compass send its

signals..amplifier/dgi etc

1 question on taf with a miniature map asking you to

identify the airport it applies to

CDMVT 2-3 q

bearing 2-3 q.. NDB bearing & qdm etc given

what does attitude indicator indicate after straight level

flight 180 deg turn...

load factor in a turn

stall speed stall speed stall angle stall angle VMU VMU

speed ...direction ....new latitude of place

Lambert's departure Lambert's departure cp pnr cp pnr Eustachian tube Eustachian tube stress stress REM sleep REM sleep

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Q1. When an altimeter is used for SSR it is always referenced to:

A) 1013.25 hPa

B) The pressure setting in use C) QFE

D) QNH

Q2. If an aircraft is equipped with one altimeter which is compensated for position error and another altimeter which is not, and all other factors being equal:

A) there will be no difference between them if air the data computer is functioning normally.

B) At high speed the non compensated altimeter will indicate a lower altitude.

C) at high speed, the non compensated altimeter will indicate a higher altitude.

D) ATC will get an erroneous altitude report SSR. Q3. VLO is defined as:

A) Minimum possible speed that the aircraft could lift off the ground

B) The maximum speed for landing gear operation C) The long range cruise speed

D) Actual speed that the aircraft lifts off the ground Q4. The rate of climb:

A) Is the downhill component of the true airspeed B) Is angle of climb times true airspeed

C) Is the horizontal component of the true airspeed

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divided by 100

Q5.. For a single engine class B aeroplane, V2 may not be less than: A) not applicable B) 1.15Vs C) 1.2Vs D) 1.5Vs Quote:

increase in flaps will cause v2 to increase, decrease? or remain unchanged.(since Vs is the reference speed) is max cruise thrust greater, lesser or equal to max continous thrust

how does change in altitude affect specific fuel consumption(sfc) - increase, decrease, remains

constant.(increase in alt. will dec. the amount of thrust reqd. for a jet engine, so less fuel flow to the engin)e what is the best air:fuel ratio by weight for jet engines varies from 15:1(can vary)?

at which point or region of a jet engine is the pressure at its highest

the high pressure compressor?

For a given aerofoil, the AOA which results in a stall: (a) remains constant regardless of bank, load or TAS

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The stall speed of an aircraft will increase with: (c) increase in the all up weight of the aircraft

The three axis of an aircraft intersect at the: (b) centre of gravity

When approaching the stall, the separation point (c) moves towards the transition point

The primary function of the rudder, while entering a turn from straight-and-level flight, is to:

(a) overcome yaw caused by lowered aileron on higher wing

An aircraft is in a state of equilibrium in: (b) in a steady climb

Adverse aileron yaw is reduced by the use of: (b) frise type ailerons

Flying near high ground or mountains with winds in excess of 15km, you can expect strong turbulence and down draughts. What would you do to avoid damaging the aircraft and / or loosing control?

(c) slow down to manoeuvring speed and fly upwind of ridge(not sure about flying upwind)

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fog will form. What might form when the wind picks up to 15kts?

(c) stratus

Which clouds are the least likely to produce airframe icing?

(c) vertical development cloud

1. What happens when CG is ahead of CP ? ..(or something like that..)

a. downward force on tail plane b. upward force on tail plane c. no force on tail plane

d. ...

2. What would you set your transponder code (SSR) to in the even of an emergency ?

a. 7400 b. 7500 c. 7700

d. some other BS option

3. Some METAR was given .. with PROB30.. What does PROB 30 mean ?

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a. probability of 30%

b. chances of some BS occuring within next 2 hours ... c.

d. ??

4. How will an intercepting aircraft signal the intercepted aircraft that it may continue it's flight ? .. (something

like that)

a. execute climbing right 90 degree turn without being out of sight of intercepted a/c

b. overtake a/c from right c. (dont remember option) d. (dont remember option)

5. While taxiing, you notice flashing green light from tower.

What does it mean ?

6. What frequency does a low altitude radar altimeter work on ?

7. Some question related to VDF and ground equipment.

8. Some question on scale ...

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10. Select the correct statement (direct reading compass) :

a. Accuracy of compass is proportional to the vertical component of earth's mag field.

b. Accuracy of compass is inversely proportional to vertical earth's mag field.

( Switch the words vertical/horizontal and inversely proportional in the above to sentences to get option c and d)

11. What does anunciator in a Remote indicating compass indicate ?

(Dont remember the options)

12. What is the Diameter of the earth ?

13. Two questions related to altimeter setting, QNH, QFE, WNE etc

14. What is used to increase lateral stability in an a/c ? (dont remember the options .. one of them was

DIHEDRAL)

15. What are the typical values indicated wrt an a/c on an SSR display screen ... ?

... (some more questions I recall ) ... .

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16. what is metabolism ?

17. What are alveoli permeable to ? a. protein

b. gases

c. dont remember d. dont rememebr

18. What do you mean by dysbarism ?

Dysbarism - Wikipedia, the free encyclopedia

19. What would you do if your breathing rate and heart rate were high on final approach, and you were hyperventilating ??

(dont remember options .. but trust me they were comical options) 20. Some problem related to Magnetic heading, Compass heading, Deviation, Variation etc .. (CDMVT type)

21. What would happen to your airspeed indicator reading if, after flying through some volcanic ash, your pitot tube and static ports get blocked ? 22. What does an airspeed indicator display if the pitot hole gets blocked with ice, but static vent remains open ?

23. Some question related to VHF, increasing altitude and it's relationship to atmospheric attenuation.

...

24. If you're flying through rain that freezes on impact, ...

(choose the correct one)

a) You're flying near thunderstorms b) You're flying through a cold front

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d) Descending would make the ice go away from the airframe

25. Some question related to gyroscopes with a diagram.

26. How many planes of freedom does the gyro in a turn indicator have ?

27. While taxiing and making a right turn, turn coordinator indicates ... :

a) Wings to the right, ball to the left b) Wings to the left, ball to the right c) wings to the left, ball to the left d) wings to the right, ball right

28. In a right banked turn, the turn co ordinator shows wings banked right and ball to the left.

select the correct statement

a) The bank angle is too much for the amount of rudder used.

b) The bank angle is too less for the amount of rudder used ..

(errr .. dont remember the options well )

29. There were atleast 2 questions related to

GPS/GNSS/GLONASS and another question asking which of the 4 options was the most accurate system.

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30. A numerical problem related to calculating the Time of Sunset in UTC at a given place. (Geographical Co-ordinates of the place is mentioned)

31. One question related to drag curve and point of least Lift to Drag ratio.

32. Several speeds were mentioned .. ie. VMU (Max

unstick speed), VMC (min control speed), V1, Vr, V2, Vs and 4 options were given .. Correct option had to be

ticked.

options like like .. a) VMU < V1 < VS

b) V1>VS>VMC etc etc ...

(so study up on all the V Speeds !)

33. If Stalling speed for an aircraft at bank angle of 10 degrees = 60 knots, what would be it's stalling speed at 45 degree bank angle turn ?

a) 70 Knots b) 83 Knots c) 85 Knots d) 90 knots

34. An aircraft that inadvertently deviates from it's flight path should :

a) inform ATC if ETA changes by more than 10 min b) ???

c) ??? d) ???

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a) 10 min b) 20-25 min c) ?? d) ?? ... ...

A Mercator Chart on a parallel 46 deg N, the Chart

distance is 133 cms. What will be the scale factor at 36 deg N/S lat?

2. Departure questions X 2 nos. having the 1st position followed by 4 different legs in NM calculate the final

position.

3. PET and PSR questions with G/S already calculated 1 each

4. Lots of Human Factors 15 questions. 5. Metrology atleast 15 questions.

a. Metar's X 2 nos. on RVR

4 Flying @ FL 22000 decent to 4000 Ft. G/S 150 kts. what will be the ROD?

5. Mode C transponder can be operated in : A. Control airspace

B. Uncontrolled airspace and to be turned on when ATC instructs

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d. Should be on at all times while flying, but can be asked by the ATC to shut down.

6. Calculate range of 2 VOR's

7. Lambert conical chat X 2 questions. 8. CRM X 4 questions.

9. Radio aids like TCAS, SSR, Primary radar, DME atleast 8 to 10 questions.

TAS - 197 kts Course - 240 Wind - 180/30

Descending from FL 200 to FL 40

Horizontal Distance travelled - 39 NMs What is the ROD?

Q6. Regarding take-off, the take-off decision speed V1: A) Is always equal to VEF (Engine Failure speed)

B) Is an airspeed at which the aeroplane is airborne but below 35 ft and the pilot is assumed to have made a decision to continue or discontinue the take-off

C) Is the airspeed of the aeroplane upon reaching 35 feet above the take-off surface

D) Is the airspeed on the ground at which the pilot is assumed to have made a decision to continue or

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Q7. The load factor in a turn in level flight with constant TAS depends on:

A) the radius of the turn and the weight of the aeroplane B) the radius of the turn and the bank angle

C) the bank angle only

D) the true airspeed and the bank angle Q8. Given the following:

True Course: 315°

Wind velocity: 230/40 TAS: 420 knots

What is the wind correction angle and the groundspeed? (WCA / GS)

A) -6° / 415 B) +6° / 425 C) +6° / 415 D) -6° / 425

Q9. How many feet you have to climb to reach FL 75? Given:

Departure aerodrome elevation = 1500 ft QNH = 1023 hPa Temperature = ISA 1 hPa = 30 ft A) 7800 ft B) 6300 ft C) 6600 ft D) 6000 ft

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The variation in the area is 6° W and the wind is calm The deviation is 4° W

In order to follow this course, the pilot must fly a compass heading of:

A) 044° B) 058° C) 040° D) 052°

Q11. Linear acceleration can give a false impression of a:

A) climb. B) turn.

C) descent. D) spin.

Q12. Which of the following statements, if any, are correct?

Euphoria is a possible result of hypoxia

Euphoria can lead to degraded decisions in flight A) Neither.

B) 1 & 2. C) 1 only. D) 2 only.

Q13. Clear ice is most often experienced, when the outside temperature is:

A) 0° to minus 20° C.

B) Minus 5° to minus 10° . C) 0° to minus 5° C.

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Q14. FL 80, an OAT +06° C is measured. What will the temperature be at FL 130, if you consider the

temperature gradient of the Standard Atmosphere? A) -6° C

B) 0° C C) +2° C D) -4° C

Q15. FL 160, an OAT -22° C is measured. What will the temperature be at FL 90, if you consider the

B) +4° C C) 0° C D) -8° C

Q16. An approximate equation for calculation conversion angle is:

A) CA=dlong x sin Lat. x sin Long. B) CA=0,5 x dlat x sin Lat.

C) CA=(dlong-dlat) x 0,5. D) CA=0,5 x dlong x sin lat.

Q17. Using an NDB it is possible to experience which of the following errors or limitations?

A) Night effect, station interference and latitude error. B) Coastal refraction, timing error and lack of a failure warning system.

C) Coastal refraction, timing error and night effect.

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warning system.

Q18. On an EHSI display, wind velocity can be displayed in which of the following modes?

A) Map, Plan, Full ILS and Full VOR.

B) Expanded ILS, Expanded VOR, Plan and Full ILS. C) Plan, Full ILS, Expanded VOR and Full VOR.

D) Map, Expanded ILS, Full ILS and Full VOR.

Q19. Radio altitude is shown on the EADI and changes from a digital display to a circular scale:

A) below 1000 ft AGL.

B) at 1000 ft and below AGL. C) at 2500 ft.

D) at DH.

Q20. If the needle and the ball of a Turn & Slip indicator both show left, what does it indicate:

A) turn to left & too much bank. B) turn to right & too little bank. C) turn to left & too little bank. D) turn to right & too much bank.

Q21. Following 180° stabilized turn with a constant attitude and bank, the artificial horizon indicates: A) too high pitch up and too high banking.

B) attitude and banking correct.

C) too high pitch-up and correct banking. D) too high pitch-up and too low banking. Q22. The speed VLO is defined as:

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A) the speed at which the aircraft leaves the ground, not more than V2 and not less than VR

B) the maximum speed for extending or retracting the landing gear

C) the minimum speed in the landing configuration with one engine inoperative at which it is possible to maintain control of the aeroplane within defined limits whilst

applying varying power

D) the stall speed in the landing configuration

Q23. Any acceleration in climb, with a constant power setting:

A) decreases the rate of climb and the angle of climb B) improves the rate of climb if the airspeed is below VY C) improves the climb gradient if the airspeed is below VX

D) decreases rate of climb and increase angle of climb Q24. Given true track 352° , variation 11° W, deviation -5° and drift 10° S the required compass heading

isSIMILAR) A) 347° B) 005° C) 358° D) 018°

Q24. What is the advantage of the remote indicating compass (slaved gyro compass) over the direct reading magnetic compass?

A) It senses the earths magnetic field rather than seeks it, so is more sensitive.

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B) It is connected to a source of electrical power and so is more accurate.

C) It is lighter.

D) It is not affected by aircraft deviation.

Q25. From position A (04° N 030° W) an aircraft flies 600 NM due south, then 600 NM due east, the 600 NM due north, then 600 NM due west. What is the aircrafts final position in relation to A?

A) Overhead A. B) Due east of A. C) Due west of A. D) Due south of A.

Q26. On the 27th of February, at 52° S and 040° E, the sunrise is at 0243 UTC. On the same day, at 52° S and 035° W, the sunrise is at: (SIMILAR)

A) 0243 UTC. B) 0523 UTC. C) 0743 UTC. D) 2143 UTC.

Q27. The great circle track X - Y measured at x is 319° , and Y 325° Consider the following statementsSIMILAR) A) Northern hemisphere, Rhumb line track is 322° .

B) Northern hemisphere, Rhumb line track is 313° . C) Southern hemisphere, Rhumb line track is 331° . D) Southern hemisphere, Rhumb line track is 322° . Q28. On a typical computer generated SSR display the following data on a particular flight will be shown:

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A) Squawk code, Flight level , True heading, Airplane callsign.

B) Destination, Flight level , Ground speed, Airplane callsign.

C) Squawk code, Magnetic heading , Ground speed, Airplane callsign.

D) Squawk code, Flight level , Ground speed, Airplane callsign.

Q29. A DME transponder does not respond to pulses received from radars other than DME because:

A) DME only responds to the strongest 100 interrogators.

B) DME transmits and receives on different frequencies. C) it will only accept the unique twin DME pulses.

D) each aircraft transmits pulses at a random rate. Q30. An aircraft DME interrogator transmits pair of

pulses for limited periods at switch on. The transmission pattern is: (similar)

A) 15000 pps for 100 seconds, thereafter 60 pps until lock on, then 27 pps.

B) 270 pps for 100 seconds, thereafter 150 pps until lock on, then 25-30 pps.

C) 27000 pps for 100 seconds, thereafter 60 pps until lock on, then 30 pps.

D) 150 pps for 100 seconds, thereafter 60 pps until lock on, then 27 pps.

Q31. An aircraft heading 325° (M) has an ADF reading of 330° Relative. The heading to steer to intercept the

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280° track inbound to the NDB at 50° is: A) 340(M)

B) 330(M) C) 310(M) D) 320(M)

Q32. The maximum VHF range when flying at FL100 would beSIMILAR)

A) 120 nm B) 100 nm C) 85 nm D) 12 nm

Q33. An aircraft on an IFR flight in VMC experiences

radio communication failure. The aircraft is assumed to: A) Land at the destination aerodrome.

B) Return to the aerodrome of departure. C) Land at the nearest suitable aerodrome. D) Land at the alternate aerodrome.

Q34. The procedure for an aircraft that suffers

communications failure during an IFR flight in visual met conditions, should:

A) Proceed direct to its destination.

B) Maintain at last cleared level and speed for 20

minutes and then continue in accordance with the flight plan.

C) Carry out instrument approach at the nearest airfield. D) Land at the nearest suitable airfield.

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failure on an IFR flight in VMC is assumed to:

A) Continue the flight to destination aerodrome in any case.

B) Leave controlled airspace and continue the flight within uncontrolled airspace.

C) Squawk IDENT and proceed to the alternate aerodrome.

D) Continue to fly in VMC, land at the nearest suitable aerodrome, report its arrival.

Q36. Q.When acknowledging mode and code, pilot needs to:

a. Acknowledge code only

b. Acknowledge both code and mode

Q37. Q. What does series of green flashes indicate when on ground?

Q38. Q.Lift and drag depend on

a. Pressure distribution of wing aerofoil section b. cambered airfoil

Q39. While turning the aircraft the pilot moves his/her head. What effect might the pilot be exposed to.

a) Coriolis Force

Q40. Decompression is caused by: c) Nitrogen coming out of solution Q41. The Retina

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it into electrical signals.

Q42. Hyperventilation is likely to occur as a result of: B) the body attempting to compensate for a drop in partial oxygen pressure.

Q43. Generally a healthy person can compensate for the lack of oxygen with altitude upto:

10,000-12,000 feet.

Q44. Which gas diffuses from the blood to the lungs during external respiration?

Carbon Dioxide

Q45. Which illusion does linear acceleration cause? Climbing

46. 100% Oxygen without direct pressure onto the face can be used up to:

40,000 feet

Q47. When being affected by Flicker Effect, the pilot should

Turn off the strobe lights

Q49. With pulse rate of 72 beats a minute and a stroke volume of 70ml. what is the cardiac output.

5 litres a minute

Q50. A person suffering from Glaucoma will have Increased pressure of the eye

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Q51. Decompression sickness symptoms can occur

Following loss of cabin pressure at altitudes higher than 18,000 feet

Q52. The effect of carbon monoxide: Increases with altitude

Q53. Clear Ice forms at temp: Near Freezing

Q54. A passenger complains of an inflated stomach at 8,000 feet. What action would you advised the

passenger to take:

1. Unbuckle the seat belt and rub the stomach.

2. Avoid eating foods with fermentation qualities and or carbonated drinks.

3. Stand up and expel gases from the intestine. 4. Drink large amounts of water.

1,2,3 is correct 4 is false.

Q55. The metabolism of alcohol is affected by time Q56.Hyperventilation can after a long period of time lead to unconsciousness due to.

low partial pressure of oxygen to the brain

Q57. The time of useful consciousness (TUC) following loss of cabin pressurization at 35,000 feet is. 30-60sec Q58Under normal conditions which gas diffuses from the

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blood to the alveoli. Carbon dioxide

Q59. Should a pilot fly with a bad cold he/she could suffer from: Sinus Pain

Q60. Above what height night vision can start to reduce?

5,000 feet

Q61. You suffer pain in an ear on a descent should you: Level off and, if necessary climb to the level where it first occurred.

Q62. Q. An aircraft is flying over sea.FL 100.True altitude 10000ft.local QNH 1003. What can you say about the airmass over which the aircraft is flying: a. It is warmer than ISA

b. It is colder than ISA

c. Its average temperature is same as that of ISA d.The information is not sufficient

Q63. Q.What kind of precipitation is from clouds found in middle latitudes:

a. Drizzle b.Hail

c. Heavy rain with large droplets d. Medium rain with large droplets

Q64. Q.What does series of red flashes from ATC mean for aircraft in flight?

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airport unsafe to land

Q65. Q.When excessive carbon dioxide has been removed , the blood

a. becomes alkaline attaching more oxygen to haemoglobin at lungs

b. becomes acidic

Q66. Eustachian tube is to:

a. equalise pressue between middle ear and external atmosphere

b. equalise pressure between sinuses and external atmosphere

Q67. Apparent wander at 45 degrees north Q68. Rhumb line on direct Mercator:

a. Straight line

b. Convex to nearer pole Q69. Arousal:

a. Body preparedness for a difficult task

b.High level of arousal means high vigilance c. All of the above

Q70.Time taken for body to adjust to circadian rhythm if flight time exceeds 24 hrs:IS 1-1.5 HR TIME CHANGE

THEN 1 DAY

a. 1-1.5 hrs per day

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be:

a. FL 75 b. FL 80 c. FL 65 d. FL 70

Q71. Initial phase of lock on Aircraft to DME, the Aircraft's transmits at what pulses.

Q. In fever below 35 deg C. a) mental disorders, coma

b) shivering tends to cease, apathy

Q72. Hysteresis error of altimeter is due to. Q. In an unaccelerated flight weight =

Q. At 18,000 partial oxygen pressure is 1/2 of what at Sea level. what statement justifies it.

a) Oxygen 1/2 of what it is at sea level b) blood is 50% saturated with oxygen

Q73. What is random error, choose from the following example.

a) A shooter mistakenly shoots from the gun b) A shooter shoots 1 in away from the target c) Pilot put wrong info in the FMS

d)

Q74. Movement of air masses in the warm front.

Q. Heading indicator will stop rotating in the vertical plane at.

A) Equator b) 45deg Lat

(32)

c) 30deg Lat d) Poles

Q75. At medium lat Coriolis force experienced: a) 7.5deg to right

b) 15deg to left

c) 7.5 deg to the left d) 10.5 deg to the right

Q76. Range of NDB at 10 kw a) 500nm b) 100nm c) 1000nm d) 50nm Few more

increase in flaps will cause v2 to increase, decrease or remain unchanged.

is max cruise thrust greater, lesser or equal to max continous thrust

how does change in altitude affect specific fuel consumption(sfc) - increase, decrease, remains constant.

what is the best air:fuel ratio by weight for jet engines at which point or region of a jet engine is the pressure at its highest

(33)

For a given aerofoil, the AOA which results in a stall: (a) remains constant regardless of bank, load or TAS (b) varies directly with the degree of bank

(c) varies with the speed of airflow around aerofoil The stall speed of an aircraft will increase with: (a) decrease in the load factor

(b) increase in the pitch attitude for straight and level (c) increase in the all up weight of the aircraft

The three axis of an aircraft intersect at the: (a) centre of pressure

(b) centre of gravity

(c) midpoint of the datum line

When approaching the stall, the separation point (a) always stays in the same position

(b) moves rearward

(c) moves towards the transition point

(b) overcome yaw caused by lowered aileron on lower wing

(c) overcome yaw caused by raised aileron on higher wing

(34)

An aircraft is in a state of equilibrium in: (a) a steady rate 1 turn

(b) in a steady climb (c) during take off

Adverse aileron yaw is reduced by the use of: (a) vortex generators

(b) frise type ailerons

(c) boundary layer fences

(a) maintain your heading and speed (b) slow down to manoeuvring speed

(c) slow down to manoeuvring speed and fly upwind of ridge

On a cold, clear, humid night with a light wind, radiation fog will form. What might form when the wind picks up to 15kts?

(a) dew (b) frost (c) stratus

(a) middle cloud (b) high cloud

(35)

---Q14. FL 80, an OAT +06° C is measured. What will the temperature be at FL 130, if you consider the

B) 0° C C) +2° C D) -4° C

Q15. FL 160, an OAT -22° C is measured. What will the temperature be at FL 90, if you consider the

B) +4° C C) 0° C D) -8° C

answers to the above questions are as follows, if

anyone thinks any of them are wrong, please feel free to correct me

PS - sorry for not contributing any questions, the test was way too tough and the options were way too

confusing for me to recollect anything from the time i walked out of the exam hall, trust me that's no excuse 1A 2C 3B 4D 5C 6D 7C 8A 9B 10D 11A 12B 13A 14D

(36)

15D 16D 17D 18A 19B 20A 21A 22B 23A ("decrease" word is missing infront of angle of climb) 24C 24A 25B 26C 27no idea, help! 28D 29C 30D 31B 32A 33C 34D 35D 36B 37continue to taxi until holding short for take off 38B 39spatial disorientation - option not present 49what is the formula to calculate this? 62A 63A 65A 66A 68B 69C 70FL80 71"intense sweating" - option not present 72A 73B 74warm air will override cold air 74D 75A 76C

anyone knows the answers to the extra questions posted? thanks

An aircraft has to communicate with a VHF station at a range of 300 nm, if the ground station

is situated 2500' amsl which ofthe following is the lowest altitude at which contact is likely to

be made? a) 190' b) 1,378' c) 37,600' d) 84,100'

Range (nm) = 1.25 sq root ht. of transmitter + 1.25 sq. root ht of reciever

300 =1.25 sq root 2500 + 1.25 sq root ht of rec. 300 = 62.5 + 1.25 sq root ht of rec

(37)

237.5 =1.25 sq root ht of rec

237.5/1.25= sq. root ht of rec ( Assume this to be X feet amsl )

190 = sq root x sq. both sides x= 36100 feet

Hence, the close option is c

Vs<V1< VR< Vmu <V2

Given

TAS = 140

True Heading = 302 W/V = 45(T)/45Kt

what is the Drift angle and Ground Speed?

.De Compression Sickness is related with 1. Henry's Law

2. Dalton Law 3. Boyle Law 4.Charles law

DME Accuracy is + - 0.2nm as per the latest ICAO Annex ;

( and 0.25 nm + 1.25 % of range for older aircraft, older than 1989)

(38)

Frangible = brakeable (easily broken)

How does leading and trailing edge flaps affect critical angle of attack ?

Why is Vmcg determined with nosewheel steering disconnected ??

The lift coefficient (CL) of an aeroplane in steady

horizontal flight is 0.42. An increase in angle of attack of 1 degree increases CL by 0.1. A vertical up gust

instantly changes the angle of attack by 3 degrees. The load factor will be:

1.71 1.49 2.49 0.74

Q-An aeroplane performs a steady horizontal turn with a TAS of 200 kt. The turn radius is 2000 m. The load

factor (n) is approximately: a)1.1

b)1.4 c)1.8 d)2.0

What are the basic elements transmitted by NAVSTAR/GPS satellites?

(39)

offset of the satellite clock from GMT i ephemeris data

ii health data

iii ionospheric delays iv solar activity

A) i, ii, iv B) ii, iii, iv

C) i, ii, iii, iv, v D) i, ii, iii

Two identical turbojet aeroplanes (whose specific fuel consumption is assumed to be constant) are in a

holding pattern at the same altitude. The mass of the first one is 95 000 kg and its hourly fuel consumption is equal to 3100 kg/h. Since the mass of the second one is 105 000 kg, its hourly fuel consumption is:

A) 3787 kg/h B) 3426 kg/h

C) 3259 kg/h (Mark scheme answer) D) 3602 kg/h

Human Performance = 12-15 ques.

2) Theory of Flight = Lot of questions of difficult standard.

3) Met = 5-6 ques 3) Regs = 8-10 ques

4) Flight Instruments = Around 10. 5) Radio aids = 10-12

(40)

6) Gen. Nav = Around 20

Met --> Met ques were not easy and they were based on JAA.

Eg. Mountain wave, Polar air mass, Freezing fog etc.

Regs --> Easy.

Eg. Transponder Codes, Airport signs, Interception signals.

Human Performance --> In-Depth Knowledge reqd. Flight Instruments + Radio Aids --> ques were

simple.

Gen. Nav --> 20% questions were tricky.

Theory of Flight --> 50% question were moderate and rest 50% question

were tough.

I hope this helps ppl who will sit fr Indigo cae in the following months...these are a few questions dat i remember from my exam on the 22nd :

Regulations:

1.What does a red flare in the air mean?

Ans:Not withstanding previous instructions do not land.

2.Visibilty,cloud minimas for VFR as well as IFR? 3.Flashing green on ground?

(41)

Ans:Continue/Clear to taxi.

4.A simple question on the semicircular system...ur heading was given so find the FL at which u can fly/ 5.Transponder codes for radio failure and unlawful interferance.

and a couple of other easy questions on regs. Human Factors:

1.Three layers of eye?

Probable ans:Iris,Cornea and Pupil

remaining all questions were from oxford human performance book.(around 10 of them)

Principles Of flight:

1.Relation between lift and drag wrt to aoa??

2.Relation between lift and weight in unaccelarated climb?

3.A question on load factor.(in a turn) 4.relation between v1,vmc,vr,v2(this is a performance question but this was the only question from performance)

1.QNH of aerodrome-1003...elevation 1500feet...u have to climb to FL75..so how much are u actually climbing.(just remember FLis always at 1013.25) Basic questions on Dme range and frequency(U r 750 nm from station at night what frequency should u use??(I think the lowest in the MF band should be

(42)

the answer)

1) Squak for radio failure.

2) DME slant range is 12 nm, a/c absolute

altitude 9000msl, DME stn height x msl, what is the error is measured slant range

3) If there is misunderstanding due to

“uncommon language” b/w controller and pilot

what instruction will be issued for the a/c to make him land

4) Vitamin A causes loss of night vision due to ? 5) Some echoes are received 30 deg left of a/c track, Mag heading of a/c is 020 (M), variation, drift provided. Plot true bearing of the echoes? 6) Divergence Is associated with?

7) One metar ques asking , formation of due at night will be most profound in which case?

8) Unlawful interference, squak code? 9) Red flares shot from tower means ?

10) Tower shoots flashing red light, what does it mean ?

11) Anti-collision light should be ON during ? 12) One performance ques asking relation b/w V1,Vmu,Vmca ?

13) During descend pilot will descend on Mach no or CAS ?

14) Relation b/w TAS and IAS as you climb or descend?

15) Standard atmosphere is defined by (couple of options given)

(43)

17) Occluded front is formed when ? 18) Night vision is affected when ?

19) Stall speed given and a/c wt 6850 lbs what will be the stall speed when a/c wt is 5000?

20) Effect of camber in longitudinal stability? 21) Effect on landing distance when a/c is on ground effect?

22) You deploy flaps when coming in to land, this behavior results from which type of knowledge (options : skill based, rule based, knowledge based, pressure based)?

23) Stereoscopic vision is? 24) Lassaire-fair cockpit ? 25) What is white out?

26) One on “seat of pants” when in IMC?

27) Illusion created by linear acceleration in IMC condition?

28) Function of semi-circular canals in ear ? 29) Pilot decided to divert from his route

30) Static stability leads to… (couple of options related to positive, negative, static dynamic stability)

31) Scale in lambert conical, contracts b/w std parallel and expands outwards from it.

32) Latent mistake causes (options given) 33) REM sleep relaxes _____ and slow wave sleep relaxes _____?

34) Effect of camber on longitudinal stability? 35) A pilot is going from A to B, at some point P he decides to divert . he has three options C,D,E.

(44)

(distance to C,D,E and HW/TW component was provided) find the destination which takes least time. TAS also given.

36) Pilot goes from A to B and back. TAS is 360 kts and HW is 60 kts. Find the time?

37) NDB allotted freq is?

38) Some freq was given and ques asked which cat will it fall in(VLF,LF,MF,VHF…)?

2) 1 what happens to lift and drag(separate ques) as

a plane climbs at const ias

2 a/c cruising at .84 mach at some altitue with time of departure and time of arrival given.it is required to delay its eta by 2 mins. when should it reduce its speed. (NOTE: the reduced speed is not given)

3 2 questions regarding intercepting and intercepted a/c

4 1 ques on rem sleep 5 astigmatism is?

6 stress is .... 4 options were given

7 an a/c is flying at a range of 750 nm on 320 fL which frequency should be used during night for r/t vhf,hf,mf,lf

(45)

height of a/c and that of antennae is given

9 simple ques to calculate g/s and wca using cx2 10 coldest air in a cold front is where?

11 principle of vor

12 principle and frequency band of ssr 13 3 ques asking the squawk code

7500,7600,7700

14 when cold front moves what happens to the stability of air ahead

15 what is vso 16 what is vlo

3) what does a red flare indicate to an a/c

-squawk code Mode A for radio faliure

-green flashes from light signals to an a/c on the ground

-if equipped with transponder facility, when should it be used?

-Transponder code '2000' Mode A is for ... -clearance of the a/c above hilly terrain,

congested area(along with the radius)

-clearance from clouds in class B airspace, abv 10,000MSL

(46)

-DME working rinciple qstns

-Meterology: TAFs, fronts, cloud types(shapes) -rate of turn, load factor qstns

-1sm= ... '

-NAVIGATION PROBLEMS:

mach no., departure, CDMVT, Track-Hdg-drift, S=D/T, freq-wavelength

numerics, scale, temp deviation, VOR indicator, line of sight range

-how does a RL appear on a direct mercator chart?(staright line)

-gyro errors, pitot-drain hole blockage -TCAS principle(transponders)

-radio altimeter(system error)

-avg. height/temp of tropopause in summer/winter

-a while dumbell indicates ... -right of way

-Human Factors (in depth,as usual) -formation of hill fog

-lapse rate, density altitude, pressure altitude -turning errors, altimeter errors

-correlation betn Vs,V1,V2,Vmc,Vlof,Vr,Vmu(< > =)

-what is the overall appearance of the a/c when the speed is reduced, and the altitude maintained -factors affecting stall speed increase/decrease -CL can be increased by.... (flaps and angle of attack)

-lift-weight relation in an unaccelerated climb __________________________________

(47)

4) If aircraft stalling speed is 74 kts, gross weight

6500 kg,what is the stalling speed with gross weigth 5000kg?

A)57 B)67 6)74 D)91

ncrease in flaps will cause v2 to increase, decrease or remain unchanged.

is max cruise thrust greater, lesser or equal to max continous thrust

how does change in altitude affect specific fuel consumption(sfc) - increase, decrease, remains constant.

what is the best air:fuel ratio by weight for jet engines at which point or region of a jet engine is the pressure at its highest

For a given aerofoil, the AOA which results in a stall:

(a) remains constant regardless of bank, load or TAS

(b) varies directly with the degree of bank

(c) varies with the speed of airflow around aerofoil The stall speed of an aircraft will increase with:

(a) decrease in the load factor

(48)

(c) increase in the all up weight of the aircraft

The three axis of an aircraft intersect at the:

(a) centre of pressure

(b) centre of gravity

(c) midpoint of the datum line

When approaching the stall, the separation point

(a) always stays in the same position

(b) moves rearward

(c) moves towards the transition point

(b) overcome yaw caused by lowered aileron on lower wing

(c) overcome yaw caused by raised aileron on higher wing

An aircraft is in a state of equilibrium in:

(a) a steady rate 1 turn

(b) in a steady climb

(c) during take off

Adverse aileron yaw is reduced by the use of:

(a) vortex generators

(b) frise type ailerons

(49)

(a) maintain your heading and speed

(b) slow down to manoeuvring speed

(c) slow down to manoeuvring speed and fly upwind of ridge

On a cold, clear, humid night with a light wind, radiation fog will form. What might form when the wind picks up to 15kts?

(a) dew

(b) frost

(c) stratus

(a) middle cloud

(b) high cloud

hey guys in today's attempt 13 ppl passed...im jst postin few ques n topics rem...hope dt wil b of sum help to any1 bt basically everyday d main topics in d xam r changin.... Nav-inst-radio

1.accuracy of DME

2.radio altimeter measures ?? a)true altitude

b)true height

c)2 more irrelevant opns.. {thr were 2 same ques}

(50)

4.on SSR whr is transponer nd interrogator? 5.VSI operates coz of difference in

a)static b)dynamic c)total

6.LSS in troposphere?

7.VSI blocked during descent

8.2 ques on acceleration/deceleration error 9.one ques on turning error

10. RIC ques

11.speed of sound depends on? 12.circumference of earth

13.circumference at 60N

14.ques to calculate radius of cone of confusion

15.if u travel at some speed on circumference of equator at some tym...hw much speed u shud travel at 60 deg lat to travel at same tym.

speed at equator was given 16.

R/T ques

1.readability 5 means? 2.phrase monitor

3.phrase go ahead 4.some basic radio call MET

1.height of high clouds 2.high clouds are

a.cirroform b.cumuliform

two more optons i dnt rem

3.sfc temp +10 deg C dew point temp +15 deg C.. wt will b the base of cloud?(ans 2000 feet)

4.2 ques related to subsidence lost comm

alot of CG ques Vfe

rate of turn/radius of turn thats al i rem....

all the best

Ques: Aircraft flying at 6000' enters cone of confusion.wht is the diameter of the cone in (nm)

Ans : VOR Cone of confusion

(51)

6000'/6080'=0.98 nm 0.98 x tan 50 = 1.16 nm

so diameter = 1.16 x 2 = 2.3 nm TAN 0 = PERPENDICULAR/BASE Angle is 50 degrees

Base is the altitude of a/c

Perpendicular is the radius of cone of confusion

I need help regarding solving of these questions,i am not able to get the concept to solve these meteorology problem,i would really appreciate if some one could help me out in these concepts

Q1. MSA given as 12000ft, flying over mountains in temperatures +9*c ,QNH set as 1023.what will the true altitude when 12000 ft is reached?

a. 11,940 b. 11,148 c. 12,210 D. 12,864

ANS -D{...how plz explain...}

Q2.Flying at FL135above the sea, the Radio altimeter indicates a true altitude of 13500ft. the local QNH is 1019hpa.hence the crossed air mass is on average, a. At ISAstandard atmospher

b. Colder than ISA C. Warmer than ISA

D. There is insufficient information ANS-B{...why plz explain...}

Q3. You are flying at FL160 with an OAT OF -27*C.QNH is 1003 hpa. what is your true altitude? a.15540 ft b.15090 ft c.16330 ft d.15730 ft ANS-B{...how plz explain...}

Q4. What is approximate vertical interval which is equal to a pressure change of 1hpa at an altitude of 5500m? a. 8m{27ft} b. 32m{105ft} c. 64m{210ft} d. 15m{50ft} ANS-D{....how plz explain...}

(52)

ANSWERS

1) When the temp. at a give alt is not ISA you need to make corrections to the indicated altitude to get True altitude.

The correction is for every 10*C above/below ISA you need to apply (add/sub) a correction of 4% to the Indicated altitude to get the true altitude.

ISA dev at 12000 ft = actual (9*C) - ISA (-9*C) = 9+9 = 18*C 10*C= 4% correction so 18*C = 7.2 % correction

7.2% of 12000 = 864ft

So since the temp at the given altitude is above ISA add the correction of 864ft to the indicated altitude of 12,000ft.

So the answer is 12,000+864 = 12,864ft.

3) Again similar to Q no.1. Since ISA deviation here is -10*C you will need to subtract 4% of 16000ft from16000ft which is 16000-640 = 15360.

Now since you are flying at FL 160 you will have set the altimeter setting as 1013.25. And your true altitude is based on your QNH which is 1003. So you will have to make an additional correction i.e 1003-1013 = -10 x 27 (1mb = 27ft) = -270

So finally true altitude = 15360-270 = 15090.

4) There are some fixed values given is some books as to the how the value of 1mb changes from S.L upto 40,000 ft.

From what I can recall for every 1 hpa the change in ht. varies like this: @ S.L= 27ft, @ 2,000ft = 30ft, @20,000ft = 50ft and @ 40,000ft = 100ft

5500m = about 18,000 ft so the closest answer is 50ft.

Sorry about Q no.4.. I'm not really good at explaining stuff as you can see. I'm not able to explain it in words. Perhaps if I could draw I could explain it better. But I will try to put it in words and get back.

Readability 2 means readable now n then

2.I understand and will comply with the message- a.Roger ( Answer) b. Wilco 3. Marshall's signal to apply brakes

4. An aircraft is intercepted by another aircraft,what frequency you will communicate this on- a. 121.5 Mhz to 243 Mhz b. 121.5 mhz to 125.5 mhz

(53)

6. Accuracy of DME is a. + - 0.5 NM b. Increases as aircraft is flying at closer range 7. DME is able to discriminate between pulses intended for itself and for other a/c coz it rejects the pulses not synchronized with its own random PRF

8. Flashing green lights to a/c already taxing on ground

means-9. Whiteout means a. A/c is flying over a snow covered lake and related options 10.ILS Cat III (a) RVR is a. 200 mts b. 250 mts

11. theta =3 degree TAS=100 kts ROD=** ANS: 500 feet/minute

12.TCAS operation uses a. transponder replies from other a/c b. a special system installed on board

13.DME uses frequency a.1000 MHZ b. 100 Mhz c. 100 KHZ

14.Question related to Primary and Secondary Radar. Primary radar relies on target reflection and secondary radar on transponder replies

15. Which is the most prominent error of NDB - Quadrental Error

16.A signal is received after fading at the receiver,Which is the most likely reason a.Quadrental Error b. Night effect c. mountainous/terrain effect d. Coastal error 17.90% of water vapour is present in a. troposphere b. lower stratosphere

18. A-B 90Nm Along the track 60 nm from A, aircraft is positioned 4nm to right.What is the correction required to track directly to B a. 12 left b. 8 left

19.NDB frequency a.190-1750 KHZ

20.Which of the following is present in Middle Ear a. Embolym b. Ossicles c. Semi-circular canal d. vestibular apparatus

21. VLE speed is a. the landing gear speed with full safety and related options 22.Blue line speed is a. Vyse b. Vmc c. Vne d. Vmo

23.mach No. Definiton

24. Divergence brings in what kind of weather

25. Echoes are received 30 degree to left.A/c hdg is 120 M , Find QTE?

26. Convergency. SH, C.A.=7, P-Q=95 Degree GC ,P-Q RL=? Ans is 088 Degree 27. Perihelion occurs a. Beginning of January b. Beginning of July

28.Civil twilight a.6 degree below the celestial horizon 29.Lines joining places of equal variation are ISOGONALS 30.Class B airspace Met Minima above 10000 feet

31.Met minima for 4500-9000 feet outside controlled airspace

32.A (45N 10 W)and B(48*30** N 15 W) Find the A-B RL track a. 300 b.330 c.345 33.a. ND shows flight director bars

b.PFD is the main flying instruent

c.Altitude information is displayed on PFD d.FMA related option

Combination of correct answers was given 34.Stage 2 sleep comprises of 50% of sleep. 35.100% Acuity is achieved at FOVEA

36.On reaching the saturation vapour pressure, a. it will stay at the same temperature b. it will become colder c. it will become warmer

37. An a/c has been hijacked and is asked to commence a descend,It cannot notify ATC of its actions. a. It will fly an Emergency triangle b, Declare emergency c. Descend to an altitude which is at a deviation of 1000 ft wen flying FL290 above and 500fr if below FL290

38.Time of Useful consciousness at 35000feet is-39, What SSR code is used for Emergency- 7700

40.An aircraft flyign with left static port blocked will- a. over read when side slipping towards port b. overread when side slipping towards starboard

(54)

41.Airfield is 0 metres above MSL,OAT is not given.QNH = 1022 HPa , QFF=? a. Less than 1022 b. more than 1022 c. 1022 d. Information is not sufficient to determine 42.One or more several static ports have been blocked on board a unpressurised aircraft.Correct remedial action will be- break the glass of Rate of climb indicator 43.Upsloping runway will give an illusion of - ??

44. Worload is defined as- a.90% of crew resources have been utilized b. 60% of crew resources have been utilized c. Depends on Pilot expertise d. Availability of resources Combinations of answers is correct

45.Myopia is- a. Nearsightedness b. Farsightedness

46.NDB signal transmits a signal pattern in the horizontal plane which is a. omni-directional b. Bi-lobar pattern c. Cardiod balanced at 30HZ freq.

47.Physiological gases are a. O2 and CO2 b. O2 and CO , Two more combinations were given

48.Ice on the aircraft surfaces will increase the landing distance by a. 40-50% b. 30-40% c.10-15%

49.Stress management is

50.With respect to CO which of the following statements is correct- a. it has 5 Times affinity to attach with hemoglobin than oxygen b. It causes Hypoxia

51.100% oxygen corresponds to the FL of a. 10000 b. 4 0000 52. Cognitive Stress

is-53. On a 5 dot indicator, an a/c is flying at a range of 100Nm on a airway. How many dots will correspond to the deviation? a.1.5 dots b.2 dots c.3 dots

54.A pilot experiences bends in joints after the Flight, a. Seek Aviation Medical Assistance immediately b. Ignore as it will get better with time

55.Tidal Volume is- Answer is 500ML

56. To prevent Vertigo- Avoid rapid head movement during the turns

57. A ( 004N 30W ) aircraft flies 600 NM south then 600 NM east, 600 NM north, 600 NM west. Aircraft's present position is?

58. When acknowledging mode and code pulse from ATC,pilot will reply by a. Repeating both mode and code pulse b. repeat only code pulse

59.Variation is applied at beacon on VOR and at A/C for NDB.

60.FL 150 , TAS=250 Kts , OAT= --12Degree Icing will occur- a. Over flat terrain,away from fronts,moderate to severe Mixed Ice b. Pushed by clouds against the

mountains,moderate to severe Mixed Ice c. Moderate to severe Rime Ice

61.A/C magnetic hdg is 120, variation= 17W track is 15 degree to the left of HDG. NDB bears (given in question) ,What will be the NDB bearing to plot on a Polar stereo graphic chart?

62.A/C is going from A (QNH 1012HPa) to B (QNH 1012Hpa), the altimeter reading differs.What could be the possible reason for this? a. Aircraft is flying over a warmer airmass b. Flying over a colder airmass c. Altimeter error

63. Dew Point and Air temperature are less than 1 Degree apart, what kind of weather will occur as a result a. Fog and Stratus b. clear sky

64. CU and CB are formed due to a. Convection b. radiation 65. Fog is a.<1000 mts visibilty due to solid and ice particles b. <1000 mts visibility due to solid and liquid particles

c.< = 1000 mts due to ice and ... particles d. < 1000 due to presence of precipitation

66.Geostrophic winds are proportional to a. density if air b. curvature of isobars 66.Average height of Stratosphere is a. 11 to 50 KM b. 50 to 85 KM

(55)

some questions which i can

recall-1. What kind of illusion pilot goes under when a/c is in bank and pilot tries to pick up a pen frm ground

2.What kind of flaps are at rear of wing

3. question on v speeds....V1 Vmc V2 Vr etc.

4. If radio failure in IFR in VMC what will u do

a. continue in VMC n land at most suitable aerodrome n inform ATC b. fly accd to flight plan and select 7600A on transponder

c. ???? d. ?????

5. Series of green flashes

6. Very simple quest on PET

7. 2 questions on true heading variation magnetic correction!!

8. what type of clouds are NS ST AS ...a. convection b.Radiation c. sinking d.?????

9. Height and type of high clouds

10 Height and temp at tropopause over poles n equator

11. Questn on fohn winds

12. signal of adf is vertically/horizontally polarised to avoid diffraction/refraction/attenuation

(56)

14. What is centre of pressure

15. Min length of clearway

16. Day Blind spot is due to

a.lack of rods n cones on fovea b.overexposure to light on fovea c.lack of rods and cones on iris

d.lack of rods and cones on optic nerve

17.First step by crew when decompression happens....dont rem the options

18. DME and VOR co-located when they r ... meters apart

19. 4 quest on GPS,D-GPS

20. sum 3-4 basic questions on pitot static instruments

21. Total pressure = a. static +dynamic b. static -dynamic ....c ??? d ??? lt

22. Height of base of clouds

23. how does GC appear on polar stereographic chart

24.a pressure chart was given....v had to analyse

25. 2 questions on radiation fog (how they r formed and dissipates)

26. what of the followin r experience by student pilot a.nervousness

b.hardness of controls c.sickness n loss of sleep d...???

27. what r symptoms of hypoxia

28. what is autokinetic illusion

29. what is cocktail party effect :ugh:

30. rad alt

31. Mercator scale...length represents a distance of 90 miles at 45 degrees north...same length represents x at 30 degrees....find x